Exploratory investigation of an airfoil with area suction applied to a porous, round trailing edge fitted with a lift-control vane / Robert E. Dannenberg and James A. Weiberg.
A two-dimensional, wind-tunnel investigation has been made of the effectiveness of area suction near the trailing edge for increasing the lift of an NACA 65₁-012 airfoil modified to incorporate a porous, round trailing edge. The modified section had a thickness-chord ratio of 0.16. A thin, small cho...
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| Format: | Government Document Book |
| Language: | English |
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Washington, D.C. :
National Advisory Committee for Aeronautics,
1955.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
3498. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/3498
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| Y 3.N 21/5:6/3498 | Available Place a Hold |